Invention Grant
- Patent Title: Revolving part for a turbine test bench for a turbomachine, turbine test bench comprising said part, and method for the use of these
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Application No.: US16072929Application Date: 2017-01-24
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Publication No.: US10822978B2Publication Date: 2020-11-03
- Inventor: Aurèlien Gaëtan Delmotte , Joël Maurice Creti , Laurent Jacques Roger Jean Doublet
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pearne & Gordon LLP
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@2f24515
- International Application: PCT/FR2017/050149 WO 20170124
- International Announcement: WO2017/129892 WO 20170803
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F04D29/26 ; G01M15/14 ; F01D5/02 ; F01D21/00

Abstract:
The invention relates to a part of revolution (60) intended to be rotated, comprising a hub (62) intended to be tightly adjusted on a rotary shaft (24), and a body (14) extending radially outwards from an axial end of the hub. In order to increase the critical speed up to which the tightening can be retained, the hub (62) comprises three relatively thick annular regions (68, 66, 70) separated from one another by two relatively thin annular regions (64a, 64b), in such a way that when the part of revolution is subject to a centrifugal force (F), the two relatively thin annular regions (64a, 64b) form privileged deformation zones acting as a double pivot. Such a part can advantageously be used as a piston for balancing in a turbine test bench or in a turbomachine.
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